Casualties unknown

2004-09-21: Piper PA-32R-301 (N801SP) — Aero Atlanta Flight Center — Euharlee, GA

Euharlee, GA, US

On September 21, 2004, a Piper PA-32R-301 (registration N801SP) operated by Aero Atlanta Flight Center was involved in an aviation accident near Euharlee, GA. Investigators recorded the probable cause as: The pilot's failure to maintain adequate control of the airplane, which resulted in the pilot exceeding the design limits of the airplane and subsequent in-flight separation. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

Metallurgical examination of a PA-32R-301 that broke up in flight revealed overstress separations with upward loading on wings and downward bending on the stabilator, with no evidence of pre-existing cracking.

Flight Purpose

According to the president of Aero Atlanta Flight Center, the flight was intended for a check-out of a second flight instructor in the PA-32R-301. The flight center president noted that such a flight would typically include normal and emergency procedures, landings, slow flight, stalls, and steep turns.

Witness Observations

A witness located approximately two miles from the accident site reported hearing an airplane engine noise that sounded "wide open." The witness then heard two very loud pops, followed by silence. Another witness, who held pilot and mechanic ratings, reported that the airplane sounded "... like it was doing a loop or some kind of high G-load maneuver." Multiple witnesses reported seeing the airplane fall from the sky in pieces.

Examination Findings

Examination of the wreckage revealed no evidence of mechanical malfunction of the engine, propeller, or flight controls. The outboard sections of both wings and the stabilator were found separated. Fracture surfaces from the left wing main spar, right wing main spar, and stabilator were sent to the National Transportation Safety Board Materials Laboratory for metallurgical examination. The laboratory report stated there was no evidence of pre-existing cracking or damage, and the fracture characteristics were consistent with overstress separations. The report specified that "Fracture, damage, and deformation patterns indicated upward loading on both wings at the time of fracture" and "Fracture, damage, and deformation patterns on the horizontal stabilator indicated downward bending overstress separations."

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040924X01489. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.